Chapter 04 Rotational Motion
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The Experimental Determination of the Moment of Inertia of a Model Airplane Michael Koken [email protected]
The University of Akron IdeaExchange@UAkron The Dr. Gary B. and Pamela S. Williams Honors Honors Research Projects College Fall 2017 The Experimental Determination of the Moment of Inertia of a Model Airplane Michael Koken [email protected] Please take a moment to share how this work helps you through this survey. Your feedback will be important as we plan further development of our repository. Follow this and additional works at: http://ideaexchange.uakron.edu/honors_research_projects Part of the Aerospace Engineering Commons, Aviation Commons, Civil and Environmental Engineering Commons, Mechanical Engineering Commons, and the Physics Commons Recommended Citation Koken, Michael, "The Experimental Determination of the Moment of Inertia of a Model Airplane" (2017). Honors Research Projects. 585. http://ideaexchange.uakron.edu/honors_research_projects/585 This Honors Research Project is brought to you for free and open access by The Dr. Gary B. and Pamela S. Williams Honors College at IdeaExchange@UAkron, the institutional repository of The nivU ersity of Akron in Akron, Ohio, USA. It has been accepted for inclusion in Honors Research Projects by an authorized administrator of IdeaExchange@UAkron. For more information, please contact [email protected], [email protected]. 2017 THE EXPERIMENTAL DETERMINATION OF A MODEL AIRPLANE KOKEN, MICHAEL THE UNIVERSITY OF AKRON Honors Project TABLE OF CONTENTS List of Tables ................................................................................................................................................ -
The Stress Tensor
An Internet Book on Fluid Dynamics The Stress Tensor The general state of stress in any homogeneous continuum, whether fluid or solid, consists of a stress acting perpendicular to any plane and two orthogonal shear stresses acting tangential to that plane. Thus, Figure 1: Differential element indicating the nine stresses. as depicted in Figure 1, there will be a similar set of three stresses acting on each of the three perpendicular planes in a three-dimensional continuum for a total of nine stresses which are most conveniently denoted by the stress tensor, σij, defined as the stress in the j direction acting on a plane normal to the i direction. Equivalently we can think of σij as the 3 × 3 matrix ⎡ ⎤ σxx σxy σxz ⎣ ⎦ σyx σyy σyz (Bha1) σzx σzy σzz in which the diagonal terms, σxx, σyy and σzz, are the normal stresses which would be equal to −p in any fluid at rest (note the change in the sign convention in which tensile normal stresses are positive whereas a positive pressure is compressive). The off-digonal terms, σij with i = j, are all shear stresses which would, of course, be zero in a fluid at rest and are proportional to the viscosity in a fluid in motion. In fact, instead of nine independent stresses there are only six because, as we shall see, the stress tensor is symmetric, specifically σij = σji. In other words the shear stress acting in the i direction on a face perpendicular to the j direction is equal to the shear stress acting in the j direction on a face perpendicular to the i direction. -
Generic Properties of Symmetric Tensors
2006 – 1/48 – P.Comon Generic properties of Symmetric Tensors Pierre COMON I3S - CNRS other contributors: Bernard MOURRAIN INRIA institute Lek-Heng LIM, Stanford University I3S 2006 – 2/48 – P.Comon Tensors & Arrays Definitions Table T = {Tij..k} Order d of T def= # of its ways = # of its indices def Dimension n` = range of the `th index T is Square when all dimensions n` = n are equal T is Symmetric when it is square and when its entries do not change by any permutation of indices I3S 2006 – 3/48 – P.Comon Tensors & Arrays Properties Outer (tensor) product C = A ◦ B: Cij..` ab..c = Aij..` Bab..c Example 1 outer product between 2 vectors: u ◦ v = u vT Multilinearity. An order-3 tensor T is transformed by the multi-linear map {A, B, C} into a tensor T 0: 0 X Tijk = AiaBjbCkcTabc abc Similarly: at any order d. I3S 2006 – 4/48 – P.Comon Tensors & Arrays Example Example 2 Take 1 v = −1 Then 1 −1 −1 1 v◦3 = −1 1 1 −1 This is a “rank-1” symmetric tensor I3S 2006 – 5/48 – P.Comon Usefulness of symmetric arrays CanD/PARAFAC vs ICA .. .. .. ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... CanD/PARAFAC: = + ... + . ... ... ... ... ... ... ... ... I3S 2006 – 6/48 – P.Comon Usefulness of symmetric arrays CanD/PARAFAC vs ICA .. .. .. ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... CanD/PARAFAC: = + ... + . ... ... ... ... ... ... ... ... PARAFAC cannot be used when: • Lack of diversity I3S 2006 – 7/48 – P.Comon Usefulness of symmetric arrays CanD/PARAFAC vs ICA .. .. .. ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... CanD/PARAFAC: = + ... + . ... ... ... ... ... ... ... ... PARAFAC cannot be used when: • Lack of diversity • Proportional slices I3S 2006 – 8/48 – P.Comon Usefulness of symmetric arrays CanD/PARAFAC vs ICA . -
Mechanics 84 6.1 2D Particle in Cartesian Coordinates
A Hostetler Handbook v 0.82 Contents Preface v 1 Newton's Laws1 1.1 Many Particles ................................. 2 1.2 Cartesian Coordinates............................. 3 1.3 Polar Coordinates ............................... 4 1.4 Cylindrical Coordinates ............................ 7 1.5 Air Resistance, Friction, and Buoyancy.................... 8 1.6 Charged Particle in a Magnetic Field..................... 17 1.7 Summary: Newton's Laws........................... 20 2 Momentum and Center of Mass 23 2.1 Rocket with no External Force ........................ 24 2.2 Multistage Rockets............................... 25 2.3 Rocket with External Force.......................... 25 2.4 Center of Mass................................. 26 2.5 Angular Momentum of a Single Particle................... 28 2.6 Angular Momentum of a System of Particles ................ 29 2.7 Angular Momentum of a Continuous Mass Distribution .......... 30 2.8 Summary: Momentum and Center of Mass ................. 34 3 Energy 36 3.1 General One-dimensional Systems ...................... 40 3.2 Atwood Machine................................ 43 3.3 Spherically Symmetric Central Forces .................... 44 3.4 The Energy of a System of Particles ..................... 45 3.5 Summary: Energy ............................... 47 4 Oscillations 49 4.1 Simple Harmonic Oscillators.......................... 49 4.2 Damped Harmonic Oscillators......................... 52 4.3 Driven Oscillators ............................... 57 4.4 Summary: Oscillations............................ -
Parallel Spinors and Connections with Skew-Symmetric Torsion in String Theory*
ASIAN J. MATH. © 2002 International Press Vol. 6, No. 2, pp. 303-336, June 2002 005 PARALLEL SPINORS AND CONNECTIONS WITH SKEW-SYMMETRIC TORSION IN STRING THEORY* THOMAS FRIEDRICHt AND STEFAN IVANOV* Abstract. We describe all almost contact metric, almost hermitian and G2-structures admitting a connection with totally skew-symmetric torsion tensor, and prove that there exists at most one such connection. We investigate its torsion form, its Ricci tensor, the Dirac operator and the V- parallel spinors. In particular, we obtain partial solutions of the type // string equations in dimension n = 5, 6 and 7. 1. Introduction. Linear connections preserving a Riemannian metric with totally skew-symmetric torsion recently became a subject of interest in theoretical and mathematical physics. For example, the target space of supersymmetric sigma models with Wess-Zumino term carries a geometry of a metric connection with skew-symmetric torsion [23, 34, 35] (see also [42] and references therein). In supergravity theories, the geometry of the moduli space of a class of black holes is carried out by a metric connection with skew-symmetric torsion [27]. The geometry of NS-5 brane solutions of type II supergravity theories is generated by a metric connection with skew-symmetric torsion [44, 45, 43]. The existence of parallel spinors with respect to a metric connection with skew-symmetric torsion on a Riemannian spin manifold is of importance in string theory, since they are associated with some string solitons (BPS solitons) [43]. Supergravity solutions that preserve some of the supersymmetry of the underlying theory have found many applications in the exploration of perturbative and non-perturbative properties of string theory. -
Matrices and Tensors
APPENDIX MATRICES AND TENSORS A.1. INTRODUCTION AND RATIONALE The purpose of this appendix is to present the notation and most of the mathematical tech- niques that are used in the body of the text. The audience is assumed to have been through sev- eral years of college-level mathematics, which included the differential and integral calculus, differential equations, functions of several variables, partial derivatives, and an introduction to linear algebra. Matrices are reviewed briefly, and determinants, vectors, and tensors of order two are described. The application of this linear algebra to material that appears in under- graduate engineering courses on mechanics is illustrated by discussions of concepts like the area and mass moments of inertia, Mohr’s circles, and the vector cross and triple scalar prod- ucts. The notation, as far as possible, will be a matrix notation that is easily entered into exist- ing symbolic computational programs like Maple, Mathematica, Matlab, and Mathcad. The desire to represent the components of three-dimensional fourth-order tensors that appear in anisotropic elasticity as the components of six-dimensional second-order tensors and thus rep- resent these components in matrices of tensor components in six dimensions leads to the non- traditional part of this appendix. This is also one of the nontraditional aspects in the text of the book, but a minor one. This is described in §A.11, along with the rationale for this approach. A.2. DEFINITION OF SQUARE, COLUMN, AND ROW MATRICES An r-by-c matrix, M, is a rectangular array of numbers consisting of r rows and c columns: ¯MM.. -
A Some Basic Rules of Tensor Calculus
A Some Basic Rules of Tensor Calculus The tensor calculus is a powerful tool for the description of the fundamentals in con- tinuum mechanics and the derivation of the governing equations for applied prob- lems. In general, there are two possibilities for the representation of the tensors and the tensorial equations: – the direct (symbolic) notation and – the index (component) notation The direct notation operates with scalars, vectors and tensors as physical objects defined in the three dimensional space. A vector (first rank tensor) a is considered as a directed line segment rather than a triple of numbers (coordinates). A second rank tensor A is any finite sum of ordered vector pairs A = a b + ... +c d. The scalars, vectors and tensors are handled as invariant (independent⊗ from the choice⊗ of the coordinate system) objects. This is the reason for the use of the direct notation in the modern literature of mechanics and rheology, e.g. [29, 32, 49, 123, 131, 199, 246, 313, 334] among others. The index notation deals with components or coordinates of vectors and tensors. For a selected basis, e.g. gi, i = 1, 2, 3 one can write a = aig , A = aibj + ... + cidj g g i i ⊗ j Here the Einstein’s summation convention is used: in one expression the twice re- peated indices are summed up from 1 to 3, e.g. 3 3 k k ik ik a gk ∑ a gk, A bk ∑ A bk ≡ k=1 ≡ k=1 In the above examples k is a so-called dummy index. Within the index notation the basic operations with tensors are defined with respect to their coordinates, e. -
Symmetric Tensors and Symmetric Tensor Rank Pierre Comon, Gene Golub, Lek-Heng Lim, Bernard Mourrain
Symmetric tensors and symmetric tensor rank Pierre Comon, Gene Golub, Lek-Heng Lim, Bernard Mourrain To cite this version: Pierre Comon, Gene Golub, Lek-Heng Lim, Bernard Mourrain. Symmetric tensors and symmetric tensor rank. SIAM Journal on Matrix Analysis and Applications, Society for Industrial and Applied Mathematics, 2008, 30 (3), pp.1254-1279. hal-00327599 HAL Id: hal-00327599 https://hal.archives-ouvertes.fr/hal-00327599 Submitted on 8 Oct 2008 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. SYMMETRIC TENSORS AND SYMMETRIC TENSOR RANK PIERRE COMON∗, GENE GOLUB†, LEK-HENG LIM†, AND BERNARD MOURRAIN‡ Abstract. A symmetric tensor is a higher order generalization of a symmetric matrix. In this paper, we study various properties of symmetric tensors in relation to a decomposition into a symmetric sum of outer product of vectors. A rank-1 order-k tensor is the outer product of k non-zero vectors. Any symmetric tensor can be decomposed into a linear combination of rank-1 tensors, each of them being symmetric or not. The rank of a symmetric tensor is the minimal number of rank-1 tensors that is necessary to reconstruct it. -
Moment of Inertia
MOMENT OF INERTIA The moment of inertia, also known as the mass moment of inertia, angular mass or rotational inertia, of a rigid body is a quantity that determines the torque needed for a desired angular acceleration about a rotational axis; similar to how mass determines the force needed for a desired acceleration. It depends on the body's mass distribution and the axis chosen, with larger moments requiring more torque to change the body's rotation rate. It is an extensive (additive) property: for a point mass the moment of inertia is simply the mass times the square of the perpendicular distance to the rotation axis. The moment of inertia of a rigid composite system is the sum of the moments of inertia of its component subsystems (all taken about the same axis). Its simplest definition is the second moment of mass with respect to distance from an axis. For bodies constrained to rotate in a plane, only their moment of inertia about an axis perpendicular to the plane, a scalar value, and matters. For bodies free to rotate in three dimensions, their moments can be described by a symmetric 3 × 3 matrix, with a set of mutually perpendicular principal axes for which this matrix is diagonal and torques around the axes act independently of each other. When a body is free to rotate around an axis, torque must be applied to change its angular momentum. The amount of torque needed to cause any given angular acceleration (the rate of change in angular velocity) is proportional to the moment of inertia of the body. -
Moment of Inertia – Rotating Disk
ANGULAR ACCELERATION AND MOMENT OF INERTIA Introduction Rotating an object requires that one overcomes that object’s rotational inertia, better known as its moment of inertia. For highly symmetrical cases it is possible to develop formulas for calculating an object’s moment of inertia. The purpose of this lab is to compare two of these formulas with the moment of inertia measured experimentally for a disk and a ring. Equipment Computer with Logger Pro SW Bubble Level String PASCO Rotational Apparatus + Ring Vernier Caliper Mass Set Vernier Lab Pro Interface Triple Beam Balance Smart Pulley + Photogate Rubber Band Note: If you are also going to determine the moment of inertia of the ring then you need to perform the first portion of this lab with only a single disk. If you use both disks you will not be able to invert them and add the ring to the system. The second disk does not have mounting holes for the ring. Only the disk with the step pulley has these positioning holes for the ring. Theory If a force Ft is applied tangentially to the step pulley of radius r, mounted on top of the rotating disk, the disk will experience a torque τ τ = F t r = I α Equation 1. where I is the moment of inertia for the disk and α is the angular acceleration of the disk. We will solve for the moment of inertia I by using Equation 1 and then compare it 2 to the moment of inertia calculated from the following equation: Idisk = (1/2) MdR where R is the radius of the disk and Md is the mass of the disk. -
Newtonian Mechanics Is Most Straightforward in Its Formulation and Is Based on Newton’S Second Law
CLASSICAL MECHANICS D. A. Garanin September 30, 2015 1 Introduction Mechanics is part of physics studying motion of material bodies or conditions of their equilibrium. The latter is the subject of statics that is important in engineering. General properties of motion of bodies regardless of the source of motion (in particular, the role of constraints) belong to kinematics. Finally, motion caused by forces or interactions is the subject of dynamics, the biggest and most important part of mechanics. Concerning systems studied, mechanics can be divided into mechanics of material points, mechanics of rigid bodies, mechanics of elastic bodies, and mechanics of fluids: hydro- and aerodynamics. At the core of each of these areas of mechanics is the equation of motion, Newton's second law. Mechanics of material points is described by ordinary differential equations (ODE). One can distinguish between mechanics of one or few bodies and mechanics of many-body systems. Mechanics of rigid bodies is also described by ordinary differential equations, including positions and velocities of their centers and the angles defining their orientation. Mechanics of elastic bodies and fluids (that is, mechanics of continuum) is more compli- cated and described by partial differential equation. In many cases mechanics of continuum is coupled to thermodynamics, especially in aerodynamics. The subject of this course are systems described by ODE, including particles and rigid bodies. There are two limitations on classical mechanics. First, speeds of the objects should be much smaller than the speed of light, v c, otherwise it becomes relativistic mechanics. Second, the bodies should have a sufficiently large mass and/or kinetic energy. -
Center of Mass Moment of Inertia
Lecture 19 Physics I Chapter 12 Center of Mass Moment of Inertia Course website: http://faculty.uml.edu/Andriy_Danylov/Teaching/PhysicsI PHYS.1410 Lecture 19 Danylov Department of Physics and Applied Physics IN THIS CHAPTER, you will start discussing rotational dynamics Today we are going to discuss: Chapter 12: Rotation about the Center of Mass: Section 12.2 (skip “Finding the CM by Integration) Rotational Kinetic Energy: Section 12.3 Moment of Inertia: Section 12.4 PHYS.1410 Lecture 19 Danylov Department of Physics and Applied Physics Center of Mass (CM) PHYS.1410 Lecture 19 Danylov Department of Physics and Applied Physics Center of Mass (CM) idea We know how to address these problems: How to describe motions like these? It is a rigid object. Translational plus rotational motion We also know how to address this motion of a single particle - kinematic equations The general motion of an object can be considered as the sum of translational motion of a certain point, plus rotational motion about that point. That point is called the center of mass point. PHYS.1410 Lecture 19 Danylov Department of Physics and Applied Physics Center of Mass: Definition m1r1 m2r2 m3r3 Position vector of the CM: r M m1 m2 m3 CM total mass of the system m1 m2 m3 n 1 The center of mass is the rCM miri mass-weighted center of M i1 the object Component form: m2 1 n m1 xCM mi xi r2 M i1 rCM (xCM , yCM , zCM ) n r1 1 yCM mi yi M i1 r 1 n 3 m3 zCM mi zi M i1 PHYS.1410 Lecture 19 Danylov Department of Physics and Applied Physics Example Center